FIELD: fuel systems of aircrafts.
SUBSTANCE: fuel manifold (1) is intended for communication with at least one fuel tank of aircraft. Fuel manifold (1) forms housing (2) intended for filling with fuel and having internal pressure P1, which is higher than internal pressure P2 of fuel tank. Housing (2) comprises at least one upper wall (3) and at least one side wall (4a) provided with bypass openings (7), intended for communication with fuel tank. Collector (1) comprises means (10, 11) for release of air bubble (6) caught between upper wall (3) and level of bypass holes (7) into fuel tank.
EFFECT: reduced risk of fuel ignition.
4 cl, 2 dwg
